TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -10°C WEIGHT® 12,000 POUNDS 10,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 10 5 83 630 1260 232 230 83 630 1260 233 231 2000 6 1 83 612 1224 232 236 83 611 1222 233 237 4000 2 -3 83 595 1190 230 240 83 595 1190 231 241 6000 -1 -7 83 581 1162 227 245 83 580 1160 228 246 8000 -5 -11 83 568 1136 225 250 83 568 1136 226 251 10,000 -9 -15 83 557 1114 223 255 83 557 1114 224 256 12,000 -13 -19 83 546 1092 221 260 83 546 1092 222 262 14,000 -16 -23 83 537 1074 219 266 83 536 1072 221 268 16,000 -20 -27 83 528 1056 217 272 83 528 1056 219 274 18,000 -24 -31 82 516 1032 214 277 82 516 1032 216 279 20,000 -27 -35 78 491 982 208 278 78 492 984 210 280 22,000 -31 -39 74 463 926 201 278 74 464 928 203 280 24,000 -35 -43 69 435 870 194 277 69 436 872 196 280 26,000 -39 -47 64 406 812 186 276 65 407 814 189 279 28,000 -44 -50 59 377 754 178 273 60 378 756 181 278 29,000 -46 -52 57 363 726 174 271 57 364 728 177 276 31,000 -50 -56 52 336 672 165 267 53 337 674 169 274 33,000 -54 -60 47 309 618 155 262 48 311 622 160 270 35,000 -58 -64 43 282 564 144 253 43 284 568 151 264 BT058812 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7A-42.  Maximum Cruise Power at 1700 RPM - ISA -10°C (Sheet 2 of 2) 7A-63